1. Libya
  2. Aircraft
  3. Su-22M Fitter F

Basic Information

Category Fixed Wing Type Attack
Year Commissioned 1981 Year Decommissioned 0
Agility 2.5 Damage Points (DP) 5
Empty Weight 10880 kg Max Weight 19500 kg
Runway Information 451-900m TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical No
Payload Weight 0 kg Crew 1 people

Aircraft Capabilities

Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles) Bombsight - Ballistic Computing

Sensor Parameters

Model Purpose Range Scan Interval Generation
SPO-10 Sirena-3M RWR, Radar Warning Receiver 0.00 - 120.00 nm 5 sec Early 1970s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
SPO-10 Sirena-3M SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2 是

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
S-5K 57mm Rocket   x 192
S-5K 57mm Rocket   x 192

Signatures

Type Front Side Rear
Visual Detection Range 3.1 nm 6.31 nm 3.1 nm
Visual Classification Range 1.7 nm 3.55 nm 2.84 nm
Infrared Detection Range 3.1 nm 8.07 nm 13.31 nm
Infrared Classification Range 1.7 nm 3.55 nm 1.7 nm
Radar, A-D Band (30-2000 MHz) 7.1 dBsm (5.13 m²) 9.4 dBsm (8.71 m²) 7.1 dBsm (5.13 m²)
Radar, E-M Band (2-100 GHz) 7.1 dBsm (5.13 m²) 9.4 dBsm (8.71 m²) 7.1 dBsm (5.13 m²)

Default Configuration

Model Comments
30mm NR-30 x 2 [80 rnds x 2] Aircraft, Su-17

Datalink

Type Model Range Channels
Radio UHF/VHF Radio [Unsecure] 100 nm 0
Radio HF Radio [Unsecure] 300 nm 10

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
1x AL-21F-3 Turbojet 1 7800 11200 0.86 1.86 No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 3740